Thales FMGS - Page 145

FLIGHT PHASES
TAKE-OFF 3
3.1. SWITCHING CONDITIONS
The FMGS transitions automatically from the PREFLIGHT phase to the
TAKE-OFF phase when the following conditions are met:
− Thrust levers set to the FLEX or TOGA detent, and,
− Left and right N1 > 85% for CFM engines, or,
− Left and right EPR > 1.25 for IAE engines, or,
− Ground speed > 90 kt.
FMA displays MAN TOGA or MAN FLEX XX or MAN DTO.
PERF & PROG pages: title field becomes TAKE OFF green and non
modifiable values switch from blue to green.
MAN
FLX 55
RWY
NAV
1FD2
A/THR
SRS
CLB
TAKE OFF
V1 FLP RETR RWY
141 F=150 14R
VR SLT RETR TO SHIFT
141 S=192 [M][ ]*
V2 CLEAN FLAPS/THS
143 O=216 2/UP0.6
TRANS ALT DRT TO-FLX TO
5000 F55
THR RED/ACC ENG OUT ACC
1990/3490 1990
UPLINK NEXT
<TO DATA PHASE>
TAKE OFF
V1 FLP RETR RWY
141 F=150 14R
VR SLT RETR TO SHIFT
141 S=192 [M][ ]*
V2 CLEAN FLAPS/THS
143 O=216 2/UP0.6
TRANS ALT DRT TO-FLX TO
5000 F55
THR RED/ACC ENG OUT ACC
1990/3490 1990
NEXT
PHASE>
TAKE OFF THV001
CRZ OPT REC MAX
FL360 FL370 FL383
<REPORT
UPDATE AT
*[ ]
BRG /DIST
301°/1.1 TO LFB014R
PREDICTIVE
<GPS GPS PRIMARY
REQUIRED ACCUR ESTIMATED
1.00NM HIGH 0.08NM
PREFLIGHT THV001
CRZ OPT REC MAX
FL360 FL370 FL383
<REPORT
UPDATE AT
*[ ]
BRG /DIST
301°/1.1 TO LFB014R
PREDICTIVE
<GPS GPS PRIMARY
REQUIRED ACCUR ESTIMATED
0.80NM HIGH 0.08NM
NAV
1FD2
CLB
MAN
DTO
MAN
TOGA
AIRBUS A318/319/320/321
© THALES AVIONICS S.A.
J43126AA 00